Evaluation of detailed transverse crack propagation toward thickness direction for CF/PEEK quasi-isotropic laminates under fatigue loading

Author:

TSUNODA Dai1,KOHARA Masahiro1,NODA Keita2,HOSOI Atsushi23,SUGIURA Naoki4,HAYASHI Takahiro4,KAWADA Hiroyuki23

Affiliation:

1. Department of Applied Mechanics, Graduate School of Fundamental Science and Engineering, Waseda University

2. Department of Applied Mechanics and Aerospace Engineering, Waseda University

3. Kagami Memorial Research Institute for Materials Science and Technology, Waseda University

4. Toyohashi R&D Center, Mitsubishi Chemical Corporation

Publisher

Japan Society of Mechanical Engineers

Subject

General Medicine

Reference14 articles.

1. Aymerich, F.and Found M.S., Response of notched carbon/PEEK and carbon/epoxy laminates subjected to tension fatigue loading, Fatigue & fracture of engineering materials & structures, Vol.23, No.8 (2000), pp675-683

2. Gamstedt, E. K. and Talreja, R., Fatigue damage mechanisms in unidirectional carbon-fibre reinforced plastics, Journal of Materials Science, Vol.34(1999), pp. 2535-2546

3. Hojo, M., Ochiai, S., Gustafson C.-G. and Tanaka, K., Effect of matrix resin on delamination fatigue crack growth in CFRP laminates, Engineering Fracture Mechanics, Vol.40, No.1 (1994), pp.35-47

4. Hosoi, A., Fukushima, S., Higashikata, Y., Tsunoda, D., Sugiura, N., Hayashi, T. and Kawada, H., Fatigue damage growth behavior of quasi-isotropic CF/PEEK and CF/Epoxy laminates, the 7th International Conference on Fatigue of Composites (ICFC-7) (2018)

5. Naghipour, P., Bartsch, M. and Voggenreiter, H., Simulation and experimental validation of mixed mode delamination in multidirectional CF/PEEK laminates under fatigue loading, International journal of solids and structures, Vol.48, No.6 (2011), pp.1070-1081

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